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Thermostructural Numerical Analysis of the Thrust Chamber of a Liquid Propellant Rocket Engine. [PDF]
Materials (Basel), 2022 The numerical simulation of rocket engine thrust chambers is very challenging as several damaging phenomena, such as plasticity, low-cycle-fatigue (LCF) and creep occur during its service life. The possibility of simulating the thermostructural behavior of the engine, by means of non-linear finite element analyses, allows the engineers to guarantee the
Citarella R +3 more
europepmc +7 more sources
Upper Stage Liquid Propellant Rocket Engine: A Case Analysis [PDF]
Journal of Aerospace Technology and Management, 2021 This paper provides an overview of the design and development process for the L75 liquid propellant rocket engine (LPRE) foreseen as upper stage of a satellite launch vehicle application.
Daniel Soares de Almeida +2 more
doaj +6 more sources
Development and analysis of simulation of liquid-propellant rocket engine pump head curve obtaining process [PDF]
Омский научный вестник: Серия "Авиационно-ракетное и энергетическое машиностроение", 2021 The paper describes the model of the centrifugal pump head curve obtaining process which helps in consideration of the implementation of automated systems in liquid-propellant rocket engine manufacturing.
D. A. Savchin, V. P. Nazarov
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Dataset of the experimentally measured heat transfer in the throat region of liquid rocket engine thrust chambers [PDF]
Data in Brief, 2021 About 500 experimental heat transfer data taken from the open literature and relevant to the most thermally solicited area (i.e., the throat region) of liquid rocket engine thrust chambers, are collected and manipulated. This collection is the outcome of
Marco Pizzarelli
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Determination of Cyclogram for Liquid-Propellant Rocket Engine [PDF]
International Journal of Aeronautical and Space Sciences, 2002 A vertical test stand based on launcher propulsion system was constructed and several tests for the determination of cyclogram were carried out. To make an accurate estimation, static and dynamic pressures were measured and analyzed. Especially, static pressure measurements using fast response sensors without extension tubes were used to determine ...
Dae Sung Lee +7 more
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Fundamental Concepts of Liquid-Propellant Rocket Engines [PDF]
, 2020 The engine of a rocket vehicle is a machine which produces thrust by accelerating a gas flowing through the machine. The reaction to this acceleration is the force which drives the vehicle. The amount of thrust generated depends on the mass flow rate of the gas moving through the engine and on the exit velocity of the gas from the nozzle. The gas flow,
Alessandro de Iaco Veris
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Сучасні інформаційні системи, 2022 The problem of choosing the values of the variable parameters of the digital stabilizer of the cosmic stage of a carrier rocket with a liquid-propellant jet engine and an onboard digital computer in the stabilization loop, which ensures stable movement ...
Eugene Aleksandrov +3 more
doaj +3 more sources
Liquid-Propellant Rocket Engine Throttling: A Comprehensive Review [PDF]
Journal of Propulsion and Power, 2009 Liquid-propellant rocket engines are capable of on-command variable thrust or thrust modulation, an operability advantage that has been studied intermittently since the late 1930s. Throttleable liquid-propellant rocket engines can be used for planetary entry and descent, space rendezvous, orbital maneuvering including orientation and stabilization in ...
M. J. Casiano +2 more
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Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроениеThe paper presents the results of simulation of spray and combustion processes in the liquid-propellant rocket engine chamber using the z77 reduced kinetic mechanism of chemical reactions and a hybrid method for determining spray parameters of a swirl ...
M. N. Senchev +4 more
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Nonlinear combustion instability in liquid-propellant rocket engines [PDF]
Symposium (International) on Combustion, 1971 Nonlinear combustion instability in liquid propellant rocket engines, describing unsteady combustor flow with single wave ...
Eugene A. Powell, Ben T. Zinn
openaire +4 more sources